F16C/D. FLIGHT MANUAL (2002) - page 76

 

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F16C/D. FLIGHT MANUAL (2002) - page 76

 

 

T.O. GR1F16CJ11

B848Change 3

1F-16CJ-1-1-4069A

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

MAXIMUM AIRSPEED

QUICKEST TURN

(15.0 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

3223 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

40

36

32

28

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    20,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 150

GW = 28,000 POUNDS

Figure B831.

T.O. GR1F16CJ11

Change 3B849

1F-16CJ-1-1-4102X

0.8

1.0

0

4

8

12

16

20

24

0.0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

MAXIMUM AIRSPEED

QUICKEST TURN

(11.0 DEGREES/ SECOND)

TIGHTEST TURN

(RADIUS =

4700 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

40

36

32

28

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    30,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 150

GW = 28,000 POUNDS

Figure B832.

T.O. GR1F16CJ11

B850Change 3

1F-16CJ-1-1-4070A

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

1595 FEET)

QUICKEST TURN

(21.1 DEGREES/SECOND)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

40

36

32

28

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    Sea Level

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 200

GW = 28,000 POUNDS

Figure B833.

T.O. GR1F16CJ11

Change 3B851

1F-16CJ-1-1-4071A

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

MAXIMUM AIRSPEED

QUICKEST TURN

(17.8 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

2250 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

40

36

32

28

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    10,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 200

GW = 28,000 POUNDS

Figure B834.

T.O. GR1F16CJ11

B852Change 3

1F-16CJ-1-1-4072A

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

TIGHTEST TURN

(RADIUS =

QUICKEST TURN

(14.9 DEGREES/SECOND)

MAXIMUM AIRSPEED

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

28

32

36

40

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    20,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 200

GW = 28,000 POUNDS

3223 FEET)

Figure B835.

T.O. GR1F16CJ11

Change 3B853

1F-16CJ-1-1-4103X

0.8

1.0

0

4

8

12

16

20

24

0.0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

QUICKEST TURN

(10.8 DEGREES/SECOND)

MAXIMUM AIRSPEED

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

28

32

36

40

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    30,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 200

GW = 28,000 POUNDS

TIGHTEST TURN

(RADIUS =

4701 FEET)

Figure B836.

T.O. GR1F16CJ11

B854Change 3

1F-16CJ-1-1-4073A

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

1.4

LIMIT AIRSPEED

QUICKEST TURN

(24.9 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

1060 FEET)

C

H

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

D

E

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

F

A

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

J

Turn Performance    Sea Level

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

F

28

A

B

I

A

G

Figure B837.

T.O. GR1F16CJ11

Change 3B855

1F-16CJ-1-1-4074A

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

1.4

TIGHTEST TURN

(RADIUS =

1300 FEET)

QUICKEST TURN

(22.8 DEGREES/SECOND)

LIMIT AIRSPEED

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    5000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

Figure B838.

T.O. GR1F16CJ11

B856Change 3

1F-16CJ-1-1-4075A

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

1.4

1.6

LIMIT AIRSPEED

TIGHTEST TURN

(RADIUS =

1584 FEET)

QUICKEST TURN

(20.9 DEGREES/SECOND)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    10,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

-800

28

-200

-200

Figure B839.

T.O. GR1F16CJ11

Change 3B857

1F-16CJ-1-1-4076A

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

1.4

1.6

LIMIT AIRSPEED

QUICKEST TURN

(19.1 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    15,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

1932 FEET)

Figure B840.

T.O. GR1F16CJ11

B858Change 3

1F-16CJ-1-1-4077A

0.8

1.0

0

4

8

12

16

20

24

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

1.4

1.6

LIMIT AIRSPEED

QUICKEST TURN

(17.4 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

2357 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    20,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

1.8

28

Figure B841.

T.O. GR1F16CJ11

Change 3B859

1F-16CJ-1-1-4078A

1.0

1.2

0

4

8

12

16

20

0.2

0.4

0.6

0.8

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.4

1.6

1.8

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

2883 FEET)

(15.9 DEGREES/SECOND)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    25,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

24

QUICKEST TURN

28

Figure B842.

T.O. GR1F16CJ11

B860Change 3

1F-16CJ-1-1-4079A

1.0

1.2

0

4

8

12

16

20

24

0.4

0.6

0.8

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.4

1.6

1.8

MAXIMUM AIRSPEED

QUICKEST TURN

(14.4 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

3530 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    30,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

Figure B843.

T.O. GR1F16CJ11

Change 3B861

1F-16CJ-1-1-4080A

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

28

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

0.8

1.0

0

4

8

12

16

20

24

1.8

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

1.4

1.6

QUICKEST TURN

(12.3 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

MAXIMUM AIRSPEED

Turn Performance    35,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

2.0

26

4330 FEET)

MAX AFT STICK

Figure B844.

T.O. GR1F16CJ11

B862Change 3

1F-16CJ-1-1-4081A

0.8

1.0

0

4

8

12

16

20

24

1.8

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

1.4

1.6

2.0

MAXIMUM AIRSPEED

QUICKEST TURN

(9.7 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

5509 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

26

24

22

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    40,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

MAX AFT STICK

Figure B845.

T.O. GR1F16CJ11

Change 3B863

Turn Performance    45,000 Feet

DATA BASIS: FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1F-16CJ-1-1-4082A

24

20

16

12

8

4

0

0.4

0.6

0.8

1.0

1.2

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.4

1.6

1.8

2.0

TIGHTEST TURN

(RADIUS =

QUICKEST TURN

(7.6 DEGREES/SECOND)

MAXIMUM AIRSPEED

6927 FEET)

28

MAX AFT STICK

Figure B846.

 

 

 

 

 

 

 

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